Flight Control System Design Using H.INF. Optimal Control.
نویسندگان
چکیده
منابع مشابه
Landing Approach Automatic Flight Control System Design via Reduced Order Optimal Control Law
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ژورنال
عنوان ژورنال: Journal of the Japan Society for Aeronautical and Space Sciences
سال: 1993
ISSN: 0021-4663
DOI: 10.2322/jjsass1969.41.324